As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A-SYSTEM HYDRAULIC FAILURE. COMPLETED ABNORMAL PROCEDURE. END NR 2 FLUID SHUTOFF FOR 20 MIN. LT WHEEL WELL FLAP HYDRAULIC MOTOR REMOVED AND REPLACED IAW B727 M/M 27-51-62. A-SYSTEM CASE DRAINS AND MOD FILTERS CHECKED FOR CONTAMINATION, NONE NOTED. RESERVICED A-SYSTEM WITH 5.5 GALLONS OF SKYDROL. OPS CHECKED SYSTEM WITH ENGINE DRIVEN PUMPS.